一种基于飞机总能量控制飞行速度/航迹的解耦控制系统设计新方法

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2004, Vol. 25 ›› Issue (4): 389-392.

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A New Method for Designing Decoupling Controller of Flight Speed/Flight Path Based on Total Energy Control

ZHANG Qing-zhen, AN Jin-wen

Automatic Control Department, Northwestern Polytechnical University, Xi'an 710072, China

Received:2003-07-15 Revised:2004-02-18 Online:2004-08-25 Published:2004-08-25

Abstract

Abstract: Total energy control(TEC) is a simple and effective design method for controller of flight speed/flight path. This paper proposed a new method based on controlling the amount of aircraft total energy and its distribution. This method adopt several error-feedback loops with simple PI controller to achieve good decoupling effect. Finally, digital simulations of this new control method is conducted with an aircraft on four of its typical situations, and the result validates this method's availability.

Key words: flight control, total energy control(TEC), decoupling control, integrated flight/propulsion control

ZHANG Qing-zhen;AN Jin-wen. A New Method for Designing Decoupling Controller of Flight Speed/Flight Path Based on Total Energy Control[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2004, 25(4): 389-392.

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A New Method for Designing Decoupling Controller of Flight Speed/Flight Path Based on Total Energy Control

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